Airframe structure of an aircraft or spacecraft
    41.
    发明授权
    Airframe structure of an aircraft or spacecraft 有权
    飞机或航天器的机身结构

    公开(公告)号:US08016234B2

    公开(公告)日:2011-09-13

    申请号:US11891755

    申请日:2007-08-13

    Abstract: The present invention provides an airframe structure of an aircraft or spacecraft, with: a hollow body section which can be subjected to an internal pressure; a membrane arrangement which has at least one single-part, multi-curved membrane component for sealing off the internal pressure from an external pressure which acts on the hollow body section and differs from the internal pressure; and a joining structure for a pressure tight joining of the membrane arrangement to a region of the hollow body section; wherein the membrane arrangement forms a receiving well which is accessible from outside the hollow body section, extends at least partially into the hollow body section and is for receiving a component of the aircraft or spacecraft.

    Abstract translation: 本发明提供了一种飞机或航天器的机身结构,其具有:可承受内部压力的中空主体部分; 膜装置,其具有至少一个单一部分的多弯曲膜部件,用于将内部压力与作用在中空主体部分上并与内部压力不同的外部压力密封; 以及用于将所述膜装置压缩接合到所述中空主体部分的区域的接合结构; 其中所述膜装置形成从所述中空主体部分的外部可接近的接收井,至少部分延伸到所述中空主体部分中并且用于接收所述飞行器或航天器的部件。

    METHOD OF FABRICATING A TRANSISTOR WITH SEMICONDUCTOR GATE COMBINED LOCALLY WITH A METAL
    42.
    发明申请
    METHOD OF FABRICATING A TRANSISTOR WITH SEMICONDUCTOR GATE COMBINED LOCALLY WITH A METAL 有权
    制造半导体门与金属组合的晶体管的方法

    公开(公告)号:US20100102402A1

    公开(公告)日:2010-04-29

    申请号:US12521802

    申请日:2008-01-10

    Abstract: A method of forming a field effect transistor comprising a gate formed on an insulating layer, the gate having, in a zone in contact with the insulating layer, a semiconducting central zone and lateral zones in the length of the gate, the method comprising forming a gate comprising a portion of insulating layer, a portion of semiconducting layer formed over the insulating layer, and a portion of mask layer formed over the semiconducting layer; performing an etching of the portion of the mask layer such that only a portion in the centre of the gate remains; and reacting the semiconducting gate with a metal deposited over the gate.

    Abstract translation: 一种形成场效应晶体管的方法,所述场效应晶体管包括形成在绝缘层上的栅极,所述栅极在与所述绝缘层接触的区域中具有在所述栅极长度上的半导体中心区域和侧向区域,所述方法包括形成 包括绝缘层的一部分的栅极,在绝缘层上形成的半导体层的一部分,以及形成在半导体层上的掩模层的一部分; 对所述掩模层的所述部分进行蚀刻,使得只有所述栅极的中心部分保留; 并使半导电栅极与沉积在栅极上的金属反应。

    Cylinder liner for combustion engines and manufacturing method
    43.
    发明授权
    Cylinder liner for combustion engines and manufacturing method 有权
    内燃机缸套和制造方法

    公开(公告)号:US06354259B2

    公开(公告)日:2002-03-12

    申请号:US09829610

    申请日:2001-04-10

    CPC classification number: F02F1/004 B22D15/02 B22D19/0009 F02F2007/009

    Abstract: A method for the manufacture of a cylinder liner for combustion engines and a cylinder liner which can be manufactured by the method according to the invention are disclosed. The method comprises a thermal spray-deposition, such as by an arc spray-deposition process, of a wearing layer on a supporting body and a spray-deposition of a protective or connecting layer on the wearing layer. The wearing layer comprises a hypereutectic aluminum-silicon alloy and the protective or connecting layer comprises a hypoeutectic aluminum-silicon alloy. A melt retarder of iron, for example, may be interposed between these two layers. The melt retarder comprises a higher melting temperature than the two aluminum-silicon alloys, thereby preventing the wearing layer from partially melting when the cylinder liner is cast into a cylinder bore.

    Abstract translation: 公开了一种用于制造用于内燃机的气缸套的方法和可以通过根据本发明的方法制造的气缸套。 该方法包括例如通过电弧喷涂沉积工艺的热喷涂沉积在支撑体上的磨损层和在磨损层上的保护或连接层的喷雾沉积。 磨损层包括过共晶铝硅合金,保护层或连接层包含亚共晶铝硅合金。 例如,铁的熔融缓凝剂可以插入在这两层之间。 熔融缓凝剂包括比两种铝 - 硅合金更高的熔化温度,从而防止当气缸套铸入汽缸孔时磨损层部分熔化。

    Turbine housing for an exhaust gas turbocharger of an internal combustion engine
    45.
    发明授权
    Turbine housing for an exhaust gas turbocharger of an internal combustion engine 有权
    用于内燃机排气涡轮增压器的涡轮机壳体

    公开(公告)号:US08827635B2

    公开(公告)日:2014-09-09

    申请号:US12927870

    申请日:2010-11-27

    Abstract: In a turbine housing for an exhaust gas turbocharger of an internal combustion engine with at least one spiral channel, which can be coupled into an exhaust gas flow of an exhaust tract of the internal combustion engine, and a receiving space for a turbine wheel which is disposed downstream of the at least one spiral channel and can be acted upon by the exhaust gas of the internal combustion engine passing through the at least one spiral channel of the turbine housing, there is at least one partial housing including the at least one spiral channel, and a housing module which is fastened to the partial housing and has a vane structure disposed upstream of the receiving space which also includes an attachment surface for a bearing section of the exhaust gas turbocharger. The invention also resides in an exhaust gas turbocharger with such a turbine housing as well as to a method for producing such a turbine housing.

    Abstract translation: 在用于具有至少一个螺旋通道的内燃机的废气涡轮增压器的涡轮机壳体中,所述螺旋通道可以联接到内燃机的排气管的排气流中,以及用于涡轮机叶轮的容纳空间 设置在所述至少一个螺旋通道的下游,并且可以通过所述内燃机的通过所述涡轮壳体的所述至少一个螺旋通道的排气作用,所述至少一个部分壳体包括所述至少一个螺旋通道 以及壳体模块,其紧固到所述部分壳体并且具有设置在所述容纳空间的上游的叶片结构,所述叶片结构还包括所述排气涡轮增压器的轴承部分的附接表面。 本发明还涉及具有这种涡轮机壳体的废气涡轮增压器以及用于生产这种涡轮机壳体的方法。

    NEW LIQUID PROCESSING DEVICE
    46.
    发明申请
    NEW LIQUID PROCESSING DEVICE 审中-公开
    新型液体加工装置

    公开(公告)号:US20130112622A1

    公开(公告)日:2013-05-09

    申请号:US13810154

    申请日:2011-07-13

    CPC classification number: G01N1/34 G01N1/4005 Y10T29/49826

    Abstract: The present invention refers to a device, comprising a hollow body having at least one open end and at least one barrier inside of the hollow body, which is non-permeable for liquids and solids under ambience conditions, however, becomes liquid-permeable by applying an external force like pressure, drag force or driving power to said barrier, wherein said barrier is spaced from at least one open end of the hollow body, the use of such a device for processing of a liquid sample, a method for preparation of said device and a method for isolation or purification of any biomolecules using said device.

    Abstract translation: 本发明涉及一种装置,其包括中空体,该空心体具有中空体内的至少一个开口端和至少一个屏障,在环境条件下对于液体和固体是不可渗透的,然而,通过施加 诸如压力,牵引力或对所述屏障的驱动力的外力,其中所述阻挡件与中空体的至少一个开口端隔开,使用这种用于处理液体样品的装置,用于制备所述液体样品的方法 装置和使用所述装置分离或纯化任何生物分子的方法。

    Fastening device for electronic modules on a support rail
    47.
    发明授权
    Fastening device for electronic modules on a support rail 有权
    支撑轨上电子模块的紧固装置

    公开(公告)号:US08325491B2

    公开(公告)日:2012-12-04

    申请号:US12517394

    申请日:2007-12-06

    CPC classification number: H02B1/052 H02B1/043 H02B1/0523

    Abstract: A device for fastening an electronic module on a mounting rail and an electronic module fastened with the device on a mounting rail are provided. The device has a displaceable nose, encompassing a profile of the mounting rail together with a stationary nose provided on the back of a housing of the electronic module. The displaceable nose is configured as a clamping profile of a slide. By plugging in mechanical anchorings, the device is mounted in recesses of the housing on the back of the electronic module. The device has a spring mechanism provided to support the electronic module on the housing. A clamping force of the device on the mounting rail results from a force to the slide applied by the spring mechanism. An end of the slide opposite of the displaceable nose protrudes beyond the housing of the electronic module for the manual displacement of the displaceable nose.

    Abstract translation: 提供了一种用于将电子模块固定在安装导轨上的装置和将该装置固定在安装导轨上的电子模块。 该装置具有可位移的鼻部,包括安装轨道的轮廓以及设置在电子模块的壳体的背面上的固定鼻部。 可移动的鼻部被配置为滑块的夹紧轮廓。 通过插入机械锚固件,该装置安装在电子模块背面的外壳的凹槽中。 该装置具有弹簧机构,用于将电子模块支撑在壳体上。 装置在安装导轨上的夹紧力由弹簧机构施加的滑动力产生。 与可移动的鼻子相对的滑块的端部突出超过电子模块的壳体,用于可移动的鼻子的手动位移。

    Device for sealing a rotating shaft
    49.
    发明申请
    Device for sealing a rotating shaft 有权
    用于密封旋转轴的装置

    公开(公告)号:US20110008169A1

    公开(公告)日:2011-01-13

    申请号:US12833053

    申请日:2010-07-09

    CPC classification number: B63H23/321

    Abstract: A device serves the purpose of sealing a rotating shaft for use under water. It exhibits face seals which seal a work area against the water. In accordance with the invention the face seals are constructed in the form of three slide ring pairs, wherein between the three slide ring pairs two areas (18, 21) are arranged. One of the areas is a sealing area adjacent to the water filled with a first medium and the other area is a leaking area adjacent to the work area. In the sealing area the first medium is held at a pressure level which is higher than the pressure of the adjacent water.

    Abstract translation: 一种装置用于密封用于水下的旋转轴。 它显示面部密封,将工作区域与水密封。 根据本发明,面密封件以三个滑环对的形式构成,其中在三个滑环之间布置两个区域(18,21)。 其中一个区域是与填充有第一介质的水相邻的密封区域,另一区域是与工作区域相邻的泄漏区域。 在密封区域中,第一介质保持在比相邻水的压力高的压力水平。

    EMBROIDERY HOOP
    50.
    发明申请
    EMBROIDERY HOOP 有权
    刺绣厅

    公开(公告)号:US20100313804A1

    公开(公告)日:2010-12-16

    申请号:US12813816

    申请日:2010-06-11

    CPC classification number: D05C9/04

    Abstract: An embroidery hoop (1) for a sewing machine or embroidery machine having two hoop parts, namely the lower hoop part (3) and the upper hoop part (5). The two hoop parts (3, 5) are connected to each other by a hinge that can be released without the use of tools. The embroidery material is clamped between the inner hinge element (9) on the lower hoop part (3) and the outer hinge element (15) on the upper hoop part (5). Through this measure, an embroidery material can be embroidered at any position.

    Abstract translation: 一种用于具有两个箍部分的缝纫机或刺绣机的绣花环(1),即下箍部分(3)和上箍部分(5)。 两个箍部分(3,5)通过可以在不使用工具的情况下被释放的铰链彼此连接。 刺绣材料被夹在下箍部分(3)上的内铰链元件(9)和上箍部分(5)之间的外铰链元件(15)之间。 通过这种措施,刺绣材料可以在任何位置绣花。

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